NASA NTRS · 19670050718
Flight angle of attack determined from ablative heat-shield patterns.
Abstract
Hypersonic trim angle of attack of lifting entry vehicles, correlating stagnation point values obtained from heat shield ablation and pressure distribution measurements
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Whitnah, A. M.. 1967-06-01. Flight angle of attack determined from ablative heat-shield patterns.. https://ntrs.nasa.gov/citations/19670050718
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